[fltsim.0] title=Boeing 737-200 Air Berlin USA sim=B737-200 model= panel= sound= texture=abe kb_checklists=Boeing737-400_check kb_reference=Boeing737-400_ref atc_type=Boeing atc_id_enable=1 atc_id=N2941 atc_id_color=0xffffffff visual_damage=1 ui_manufacturer=Boeing ui_type=737-200 ui_variation=Air Berlin USA description=Boeing 737-200 Air Berlin USA, registration N2941W, repaint by Alf Werner 06.03, model by FFX\/SGA atc_airline=AIR BERLIN atc_heavy=0 atc_flight_number= [forcefeedback] gear_bump_nose_magnitude=3000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=2700 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=1300 ; 0 - 10000 ground_bumps_angle1=08900 ; 0 - 35999 degrees ground_bumps_intercept1=3.0 ground_bumps_slope1=0.20 ground_bumps_magnitude2=200 ; 0 - 10000 ground_bumps_angle2=09100 ; 0 - 35999 degrees ground_bumps_intercept2=1.075 ground_bumps_slope2=0.035 crash_magnitude1=10000 ; 0 - 10000 crash_direction1=01000 ; 0 - 35999 degrees crash_magnitude2=10000 ; 0 - 10000 crash_direction2=9000 ; 0 - 35999 degrees crash_period2=75000 ; in microseconds crash_duration2=2500000 ; in microseconds [ground_reaction] main_gear_static_compression=1.0 // (feet), The distance the main gear strut is compressed when at rest on the ground center_gear_static_compression=0.8 // (feet), The distance the center gear strut is compressed when at rest on the ground main_gear_damping_ratio=0.9 // Main gear strut damping, 0 = undamped osciallations, 1 = critically damped center_gear_damping_ratio=0.9 // Center gear strut damping, 0 = undamped osciallations, 1 = critically damped [pitot_static] vertical_speed_time_constant=1 //Increasing this value will cause a more instantaneous reaction in the VSI [General] performance=Model by Jorge Oppenheimer. \nEngine's type: P & W JT8D-9A \nWing span: 93 ft\nTotal height 37 ft. \nStatic T\/O Thrust (per engine) 14500 lb. \nMax. range 2600 km \nMax. T\/O weight 117000 lb. \nCruising altitude 31 - 35000 ft. \nMax. fuel weight 34592 lb. \nCruising speed 490 m.p.h. \nMax. payload structural 30200 lb.\nCargo capacity 875 cu. ft. \nOverall length 100 ft. 2 in. \nNumber of seats 117\n atc_type=BOEING AIRCRAFT atc_model=B732 [WEIGHT_AND_BALANCE] reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= 0.000, 0.000, 0.000 max_number_of_stations=50 station_load.0=0.000, 0.000, 0.000, 0.000 empty_weight= 85000.000 empty_weight_roll_MOI= 1062809.000 empty_weight_pitch_MOI= 1411739.000 empty_weight_yaw_MOI= 1779732.000 empty_weight_coupled_MOI= 1300.000 max_gross_weight= 103759.999 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [fuel] Center1= 7.546, 0.000, 0.000, 2313.000, 0.000 LeftMain= 4.546, -19.000, 0.000, 1499.000, 0.000 RightMain= 4.546, 19.000, 0.000, 1499.000, 0.000 fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 [airplane_geometry] wing_area= 980.000 wing_span= 93.000 wing_root_chord= 10.500 wing_dihedral= 5.999 wing_incidence= 0.000 wing_twist= -0.994 oswald_efficiency_factor= 4.997 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= 0.000 wing_pos_apex_vert= 0.000 htail_area= 408.000 htail_span= 41.667 htail_pos_lon= -37.167 htail_pos_vert= 0.000 htail_incidence= 0.000 htail_sweep= 0.000 vtail_area= 305.000 vtail_span= 19.912 vtail_sweep= 0.000 vtail_pos_lon= -37.167 vtail_pos_vert= 5.833 elevator_area= 102.000 aileron_area= 39.200 rudder_area= 51.850 elevator_up_limit= 27.502 elevator_down_limit= 20.626 aileron_up_limit= 19.481 aileron_down_limit= 14.897 rudder_limit= 23.491 elevator_trim_limit= 19.481 spoiler_limit= 59.989 spoilerons_available= 1 aileron_to_spoileron_gain= 3.000 min_ailerons_for_spoilerons= 9.969 min_flaps_for_spoilerons= 0.000 [contact_points] point.0= 1.000, 32.917, 0.000, -8.300, 1181.102, 0.000, 1.219, 53.700, 0.800, 2.500, 0.900, 5.000, 5.000, 0.000, 0.000, 0.000 point.1= 1.000, -4.250, -8.580, -9.850, 1574.803, 1.000, 1.219, 0.000, 1.000, 2.500, 0.900, 6.900, 6.900, 2.000, 0.000, 0.000 point.2= 1.000, -4.250, 8.580, -9.850, 1574.803, 2.000, 1.219, 0.000, 1.000, 2.500, 0.900, 6.900, 6.900, 3.000, 0.000, 0.000 point.3= 2.000, -15.000, -46.500, 2.250, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4= 2.000, -15.000, 46.500, 2.250, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5= 2.000, -48.000, 0.000, 1.667, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6= 2.000, 34.833, 0.000, 1.667, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch= 0.000 static_cg_height= 7.791 [GeneralEngineData] engine_type= 1 Engine.0= 5.417, -15.833, -2.583 Engine.1= 5.417, 15.833, -2.583 fuel_flow_scalar= 1.000 [SMOKESYSTEM] smoke.0=5.41,-2.58,-15.8, SMOKE_JT8D smoke.1=5.41,-2.58,15.8, SMOKE_JT8D [TurbineEngineData] fuel_flow_gain= 0.004 inlet_area= 19.600 rated_N2_rpm= 29920.000 static_thrust= 15900.000 afterburner_available= 0 reverser_available= 1 [Reference Speeds] flaps_up_stall_speed= 142.000 full_flaps_stall_speed= 113.600 cruise_speed= 395.375 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [Views] eyepoint=35.832923,0.000000,4.588050 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.000000 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=90.000000 pitch_takeoff_ga=8.000000 [direction_indicators] direction_indicator.0=3,0 [TailHook] tailhook_length=4 tailhook_position=0.0, 0.0, 0.0 cable_force_adjust=0.7 [folding_wings] wing_fold_system_type=4 ;0=None fold_rates=0.12,0.11 [EFFECTS] wake=fx_wakewater=fx_spraydirt=fx_tchdr5concrete=fx_sparkstouchdown=fx_tchdwn, 1 [Flaps.0] type= 1 span-outboard= 0.500 extending-time= 30.000 system_type= 0 damaging-speed= 0.000 blowout-speed= 0.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 1.000, 0.000 flaps-position.2= 2.000, 0.000 flaps-position.3= 5.000, 0.000 flaps-position.4= 10.000, 0.000 flaps-position.5= 15.000, 0.000 flaps-position.6= 25.000, 0.000 flaps-position.7= 30.000, 0.000 flaps-position.8= 40.000, 0.000 [Flaps.1] type= 2 span-outboard= 0.000 extending-time= 6.000 system_type= 1 damaging-speed= 250.000 blowout-speed= 300.000 lift_scalar= 0.000 drag_scalar= 0.000 pitch_scalar= 0.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 1.000, 0.000 flaps-position.2= 2.000, 0.000